McDonnell Douglas A-4 Skyhawk vs. Lockheed Martin C-130J Super Hercules

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McDonnell Douglas A-4 Skyhawk versus Lockheed Martin C-130J Super Hercules
12.19 m 40 ft 0 in length 34.37 m 112 ft 9 in
4.57 m 15 ft height 11.86 m 38 ft 11 in
8.08 m 26 ft 6 in wingspan 40.41 m 132 ft 7 in
1x Pratt & Whitney J52-P-6A Jet engines 4 x Rolls-Royce AE 2100D3 turboprop engines
8,500 pound-force thrust per engine Approximately 4,700 hp per engine
8,500 pound-force total thrust Approximately 18,800 hp total
11,113 kg 24,500 lb MTOW 76,610 kg 168,900 lb
3,222 km 1,739 nm range 4,600 km 2,485 nm
586 kts 364 mph cruise speed 660 km/h 410 mph
Up to 9,155 pounds of weapons on 5 hardpoints capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.